論文- 永井 大樹 -
表示方法: 表示形式: 表示順:
件数:232件
[2012]
101.Development of Back Surface TSP Measurement Technique for Shock Interaction Aerodynamic Heating in High Enthalpy Flow.[Proceedings of 9th International Conference Fluid Dynamics,(2012)]Nishigata, K., Nagai, H., Asai, K.
102.Compressibility Effect on Aerodynamic Characteristics of Low Reynolds Number Airfoils.[Proceedings of 9th International Conference Fluid Dynamics,(2012)]Suwa, T., Numata, D., Nagai H., Asai K.
103.断層シュリーレン法を用いた超音速複葉翼の内部構造の解明.[日本航空宇宙学会論文集,60(3),(2012),142-147]萩原真澄,永井大樹,沼田大樹,浅井圭介
104.Compressibility Effect on Airfoil Aerodynamics at Low Reynolds Number.[Proceedings of AIAA Fluid Dynamics and Co-located Conferences and Exhibit,(2012)]Suwa, T., Numata, D., Nagai, H. and Asai, K.
105.Thermal Vacuum Testing of a Small Loop Heat Pipe with a PTFE Wick for Spacecraft Thermal Control.[Transactions of the Japanese Society for Artificial Intelligence, Aerospace Technology Japan,10,(2012),27-33]Nagano, H., Nishikawara, M., Fukuyoshi, F., Ogawa, H. and Nagai, H.
106.テーパ型超音速複葉翼の始動特性と翼端板効果.[日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences,60(1),(2012),1-8]藤園 崇, 山下 博, 豊田 篤, 永井 大樹, 浅井 圭介, 鄭 信圭, 大林 茂
10.2322/jjsass.60.1
107.テーパ型超音速複葉翼の始動特性と翼端板効果.[日本航空宇宙学会論文集,60(1),(2012),1-8]藤園崇,山下博,豊田篤,永井大樹,浅井圭介,鄭信圭,大林茂
108.Aerodynamic Characteristics and Effects of Winglets of the Boomless Tapered Supersonic Biplane during the Starting Process.[Trans. JSASS Space Tech. Japan,(2012)]iroshi YAMASHITA, Takashi FUJISONO, Atsushi TOYODA, Hiroki NAGAI, Keisuke ASAI, Shinkyu JEONG and Shigeru OBAYASHI
109.Characterization of Frequency Response of Pressure-Sensitive Paints.[Proceedings of the 50th AIAA Aerospace Sciences Meeting,(2012)]Sugimoto, T., Kitashima, S., Numata, D., Nagai, H., Asai, K.
110.Conceptual Design of a Miniature, Propeller-Driven Airplane for Mars.[Proceedings of the 50th AIAA Aerospace Sciences Meeting,(2012)]Fujita, K., Nagai, H., Asai, K.
111.Conceptual Design of Mars Airplane.[Trans. JSASS Aerospace Tech. Japan,10(ists28),(2012),Te_5-Te_10]Fujita, K., Luong, R., Nagai, H., Asai, K.
[2011]
112.Development of An Experimental Small Loop Heat Pipe with Polytetrafluoroethylene Wicks.[Journal of Thermophysics and Heat Transfer,25(4),(2011),547-552]Nagano, H., Fukuyoshi, F., Ogawa, H. and Nagai, H.
113.Secondary Wick Effect for Performance of Loop Heat Pipes.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),554-555]Magome, K., Nagai, H.
114.Experimental Study of Low-Reynolds-Number Aerodynamic Characteristics of Thin Airfoils in a Mars Wind Tunnel.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011)]Nagai, H., Ida, S., Nose, K., Anyoji, M., Numata, D. and Asai, K.
115.Aerodynamics Characteristics of Ishi Airfoil at Low Reynolds Numbers.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011)]Anyoji, M., Nonomura, T., Oyama, A., Fujii, K., Nose, K., Numata, D., Nagai, H. and Asai, K.
116.Design of A Propeller of An Airplane on Mars.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011)]Hayashida, T., Sunada, S., Ishida, R., Kaneko, K., Suwa, T., Nagai, H., Asai, K., Goto, Y., Yonezawa, K. and Tsujimoto, Y.
117.Comparison of Aerodynamic Data of a Wing Tested in Wind Tunnels at Low Reynolds Numbers.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011)]Koike, M., Nagai, H., Yonemoto, K. and Asai, K.
118.Evaluation of Aerodynamic Characteristics of a Triangular Airfoil at Low Reynolds Number and High-Subsonic Mach Number.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011)]Suwa, T., Nose, K., Numata, D., Nagai, H., and Asai K.
119.Aerial Deployment Test of a Small UAV for Mars Exploration Flight.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),340-341]Fujita, K., Nagai, H., Asai, K. and Tokutake, H.
120.Conceptual Examination of a Small UAV for Mars Exploration Flight.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),448-449]Fujita, K., Nagai, H. and Asai, K,
Page: [prev] [1] [2] [3] [4] [5] [6] [7] [8] [9] [10] [11] [12] [next]
戻るこのページのトップへ
copyright(c)2005 Tohoku University